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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 1161-1180 of 1393
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Factors affecting the performance of the nozzle of a hypersonic shock tube
B. D. Henshall
;
G. E. Gadd
(
1956
)
Heat transfer to turbine blades
S.J. Andrews
;
P.C. Bradley
(
1956
)
The effects of convex surface curvature on boundary layer separation in supersonic flow
G. E. Gadd
(
1956
)
Low speed static and fluctuating pressure distributions on a cylindrical body with a square flat plate airbrake
T. B. Owen
(
1956
)
An index of mathematical tables for shock-tube flow
B. D. Henshall
(
1956
)
Some notes on the flow durations occurring in hypersonic shock tubes
B. D. Henshall
(
1956
)
Fatigue loadings in flight - loads in the wing of a varsity
Anne Burns
(
1956
)
Towing tank tests to determine the water drag of the hull of a jet-propelled flying boat fighter (spec.E.6/44) and comparison with full scale measurements
R.V. Gigg
;
A.G. Kurn
;
J.K. Friswell
(
1956
)
A constructional method for minimising the hazard of catastrophic failure in a pressure-cabin
D. Williams
(
1956
)
A flight investigation of the wake behind a meteor aircraft, with some theoretical analysis
D. R. Andrews
(
1956
)
Saunders-Roe princess flying boat G-alun engineering appraisal
Aeronautical Research Council
(
1956
)
Report of the pressure panel on the definitions of quantities having the dimensions of pressure
Aeronautical Research Council
(
1956
)
Impact measurements on a large model of a representative landplane fuselage on water
J.E.Allen
(
1956
)
Water tunnel boundary effects on axially symmetric fully developed cavities
I. J. Campbell
;
G. E. Thomas
(
1956
)
Saunders-Roe princess flying boat G-alun air and water performance tests
Aeronautical Research Council
(
1956
)
Flutter calculations on a rudder with trailing-edge spoiler
Ll. T. Niblett
(
1956
)
A note on derivative apparatus for the N.P.L. 9.5-inch high speed tunnel
J. B. Bratt
(
1956
)
Base pressures in supersonic flow
G. E. Gadd
;
D. W. Holder
;
J. D. Regan
(
1956
)
Aerodynamic derivatives for two cropped delta wings and one arrowhead wing oscillating in distortion modes
D. L. Woodcock
(
1956
)
The hot-wire anemometer for turbulence measurements part 4
B. Wise
;
D. L. Schultz
(
1956
)
Now showing items 1161-1180 of 1393
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